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You searched for: (collection:ufnaca OR mediatype:ufnaca) AND -mediatype:collection AND firstTitle:A
[texts]Acoustics of a nonhomogeneous moving medium - United States.: National Advisory Committee for Aeronautics
Keywords: Nonlinear acoustics--Research
Downloads: 115
[texts]Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel - Langley Aeronautical Laboratory
Keywords: Mach number; Aerofoils; Drag (Aerodynamics; Lift (Aerodynamics; Aerodynamics--Research; Aerodynamics--Research
Downloads: 475
[texts]Aerodynamic tests of an AN-M-65-AZON 1000-pound radio-controlled bomb in the LMAL 16-foot high-speed tunnel - Langley Aeronautical Laboratory
Keywords: Aerofoils; Mach number; Guided bombs; Aerodynamics--Research; Aerodynamics--Research
Downloads: 103
[texts]Aerodynamic tests of an M-31 bomb in the 8-foot high-speed tunnel - Langley Aeronautical Laboratory
Keywords: Projectiles, Aerial; Aerodynamics--Research
Downloads: 63
[texts]Air admixture to exhaust jets - United States.: National Advisory Committee for Aeronautics
Keywords: Aerodynamics; Rocket engines--Exhaust emissions; Rocket engines--Thrust
Downloads: 166
[texts]Air-water analogy and the study of hydraulic models - United States.: National Advisory Committee for Aeronautics
Keywords: Aeronautics; Hydraulic models
Downloads: 83
[texts]Aircraft configurations developing high lift-drag ratios at high supersonic speeds - Ames Research Center
Keywords: Drag (Aerodynamics; Aerodynamics, Supersonic; Aerodynamics--Research
Downloads: 206
[texts]Airfoil measurements in the DVL high-speed wind tunnel (2.7-meter diameter) : = Profilmessungen im DVL-Hochgeschwindigkeitswindkanal (2,7-meter Durchmesser) - United States.: National Advisory Committee for Aeronautics
Keywords: Camber (Aerofoils; Aeronautics
Downloads: 88
[texts]Airfoil theory at supersonic speed - United States.: National Advisory Committee for Aeronautics
Keywords: Drag (Aerodynamics; Aerofoils
Downloads: 245
[texts]Airfoil-contour modifications based on [epsilon]-curve method of calculating pressure distribution - Langley Aeronautical Laboratory
Keywords: Aerofoils; Aerodynamics--Research
Downloads: 68
[texts]Amplitude distribution and energy balance of small disturbances in plate flow : = Amplitudenverteilung und energiebilanz der kleinen störungen bei der plattenströmung - United States.: National Advisory Committee for Aeronautics
Keywords: Aeronautics; Force and energy
Downloads: 89
[texts]Analysis of available data on the effectiveness of ailerons without exposed overhang balance - Langley Aeronautical Laboratory
Keywords: Ailerons; Aerodynamics--Research
Downloads: 122
[texts]Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes - United States.: National Advisory Committee for Aeronautics
Keywords: Aeronautics--Research; Airplanes, Tailless; Lift (Aerodynamics; Trailing edge flaps--Aerodynamics
Downloads: 89
[texts]Analysis of vertical-tail loads in rolling pull-out maneuvers - Langley Aeronautical Laboratory
Keywords: Ailerons; Aerodynamics--Research
Downloads: 96
[texts]Analytical study of shimmy of airplane wheels - United States.: National Advisory Committee for Aeronautics
Keywords: Flutter (Aerodynamics; Airplanes--Landing gear
Downloads: 125
[texts]Annual report - National Advisory Committee for Aeronautics (Volume 44(1957)) - United States: National Advisory Committee for Aeronautics
Keywords: Aeronautics--United States; Aeronautics, Military--United States; Aeronautics--United States; Aeronautics, Military--United States
Downloads: 239
[texts]Apparatus for measurements of time and space correlation - United States.: National Advisory Committee for Aeronautics
Keywords: Turbulence--Research; Aerodynamics--Research
Downloads: 73
[texts]Application of spring tabs to elevator controls - Langley Aeronautical Laboratory
Keywords: Flutter (Aerodynamics; Elevators (Airplanes; Aerodynamics--Research
Downloads: 79
[texts]Approximate determination of the power required to move control surfaces as related to control-booster design - Langley Aeronautical Laboratory
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 93
[texts]Approximate formulas for the computation of turbulent boundary-layer momentum thicknesses in compressible flows - Langley Aeronautical Laboratory
Keywords: Turbulent boundary layer; Compressibility; Aerodynamics--Research
Downloads: 92
[texts]Approximate method for calculation of the laminar boundary layer with suction for bodies of arbitrary shape - United States.: National Advisory Committee for Aeronautics
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 83
[texts]Approximate method for estimating the incompressible laminar boundary-layer characteristics on a flat plate in slipping flow - Langley Aeronautical Laboratory
Keywords: Laminar boundary layer; Aerodynamics--Research
Downloads: 72
[texts]Approximate method of integration of laminar boundary layer in incompressible fluid - United States.: National Advisory Committee for Aeronautics
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 80
[texts]Autogenous welding in airplane construction - United States.: National Advisory Committee for Aeronautics
Keywords: Aerodynamics; Airplanes--Design and construction; Oxyacetylene welding and cutting
Downloads: 229
[texts]Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane - Langley Aeronautical Laboratory
Keywords: Fighter planes; Ailerons; Aerodynamics
Downloads: 104
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